Douglas XB-43 Jetmaster

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The Douglas XB-43 project was initiated in late 1943, and was basically an all-jet powered revision of the XB-42 design. Two prototypes were built, with the first flight taking place in May of 1946. After several years of being used for testing purposes, the aircraft were retired in 1953. See the links below for more information on this aircraft.

For more data on this aircraft, click here for Joe Baugher's webpage.
USAF archives on this aircraft, click here.
Additional information on this aircraft can be found at Wikipedia here.
(updated February 2009)


Douglas XB-43 Jetmaster

Type:           jet bomber

Crew:           three

Armament:       two .50 cal machine guns in tail (never installed)

                up to 8000 lbs. of bombs 



Specifications:

        Length:         51' 5"

        Height:         24' 3" 

        Wingspan:       71' 1" 

        Wing area:      325 sq. ft (30 sq. m)

        Weight:   	40,000 lbs. (max. gross weight)



Propulsion:

        No. of Engines: 2

        Powerplant:     General Electric J35-GE-3 (TG-180) axial flow turbojets

        Horsepower:     4,000 lbs. thrust each



Performance:

        Range:          2500 miles 

        Cruise Speed:   410 mph 

        Max Speed:      503 mph 

        Climb:          2470 ft/min initial climb rate

        Ceiling:        38500 ft 

(go to Douglas page)

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